As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(LEFT WING) UPPER T/E PANEL LOWER SURFACE SUPPORT ANGLE IS CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE #1 PYLON AFT TIP / REMOVED AND REPLACED L/W UPPER T/E PANEL LOWER SURFACE SUPPORT ANGLE AT TRANVERSE WEB ATTACH POINT ABOVE #1 PYLON AFT TIP IAW SRM 51-40-02-0G-0 STEP 4. AND SOPM 20-50-01. 56839U 13DEC17